Zhang Jinsheng  , Yuan Huacheng  ,Wang Yunfei  , Huang Guoping

DOI Number XXX-YYY-ZZZ

Conference Number HiSST 2018_700868

Design of a two-dimension variable inlet operating from Mach 0 to 4 was developed in this paper to meet the specific request. Numerical simulation was carried out to investigate the aerodynamic performance and variable geometric rules of the inlet. In addition, passive control methods were used to improve the performance. The result indicated that the initial inlet basically met the design request over a wide speed range expect Ma3 and Ma3.5.Using geometric modification and suction case could improve inlet performance. In this article, the total pressure recovery σe at Ma3 increased about 9% and distortion Δσ0 decreased 80% at Ma3.5.The thicker boundary layer on the sidewall layer is the reason for the low performance of the original configuration.

Download the Full Paper >

In Categories: High-Speed Aerodynamics and Aerothermodynamics, HiSST 2018, Hypersonic Aerodynamics, Hypersonic Flight Dynamics, Materials and Structures
Email
Print
LinkedIn
The paper above was part of  proceedings of a CEAS event and as such the author has signed a publication agreement to have their paper published in the repository. In the case this paper is found somewhere else CEAS always links to the other source.  CEAS takes great care in making the correct content available to the reader. If any mistakes are found  in the listings please contact us directly at papers@aerospacerepository.org and we will correct the listing promptly.  CEAS cannot be held liable either for mistakes in editorial or technical aspects, nor for omissions, nor for the correctness of the content. In particular, CEAS does not guarantee completeness or correctness of information contained in external websites which can be accessed via links from CEAS’s websites. Despite accurate research on the content of such linked external websites, CEAS cannot be held liable for their content. Only the content providers of such external sites are liable for their content. Should you notice any mistake in technical or editorial aspects of the CEAS site, please do not hesitate to inform us.